Chair: R. Bureo Dacal & A. Carrella

Guillaumet 1

08:30 - 08:50 - Dynamic Mass Measurements to Improve Microdynamic Tests Etienne Cavro - INTESPACE
08:50 - 09:10 - Ground and on Orbit Microvibration Verification of the DMC3 1m Resolution Earth Imaging Spacecraft Constellation Guy Richardson - Surrey Satellite Technology Ltd
09:10 - 09:30 - A methodology for exchanging information at the interface for microvibrations analysis Roseline Schmisser - CNES

Chair: S. Roose & V. Koryanov

Spot

08:30 - 08:50 - Deployable Structures Activities at the European Space Agency’s Structures Section Alexander Ihle - ESA - European Space Agency, ESTEC
08:50 - 09:10 - Scalable Large Deployable Mesh Antenna Reflector Technology Demonstration Nikoloz Maghaldadze - Large Space Structures UG
09:10 - 09:30 - Design Analysis of A Deployable Reflector Consists of Tetrahedral Modules Bei Cai - Shanghai YS Information technology Co, Ltd
09:50 - 10:10 - SCALABLE: Assembly and Testing of a Large Deployable Antenna Demonstrator Paolo Zolla - HPS GmbH

Chair: R. Usinger & T. Henriksen

Cassiopée

08:30 - 08:50 - Mechanical validation plan and validation matrixes, application to constellation program structures Teribat Jérémy - ThalesAleniaSpace
08:50 - 09:10 - Numerical simulations of ergol behavior in satellite tank at low Bond numbers and under microgravity condition. Alexis Dalmon - Institut de Mécanique des Fluides de Toulouse - IMFT
09:10 - 09:30 - Mechanical analysis workflow for satellite design and sizing Nicolas Sarda - Airbus Defence and Space SAS
09:30 - 09:50 - Novel stress-based criterion for the design of adhesive-bonded space electronics Lassaad Ben Fekih - University of Mons
09:50 - 10:10 - "NORMAL-SHEAR-MOMENTS" DIAGRAMS FOR SPECIFICATION, DESIGN AND VALIDATION OF THE PRIMARY STRUCTURE OF A TELECOM SATELLITE Teribat Jérémy - Thales Alenia Space

Chair: Q. Shi & A. Grillenbeck

Guillaumet 2

08:50 - 09:10 - Repeated shocks in Solar Arrays shims during sine vibrations Anne Giovannini - THALES ALENIAS SPACE
09:10 - 09:30 - A new Integrated Tool for Test Management Paul-Eric Dupuis - INTESPACE
09:30 - 09:50 - PAZ SATELLITE ENVIRONMENTAL TEST CAMPAIGN Víctor Bautista Juzgado - AIRBUS DEFENCE AND SPACE
09:50 - 10:10 - Mechanical development and qualification of the Sentinel-3A spacecraft Robert Knockaert - ESA

Chair: S. Roose & V. Koryanov

Spot

10:40 - 11:00 - Passive Nonlinear Actuators for Deploying the Mesh Antennas Zhihua Zhihua Zhao - Tsinghua University
11:00 - 11:20 - Adaptive Thin Shell Reflectors for Future Space Telescopes André Preumont - ULB
11:20 - 11:40 - Manufacturing and Testing of a 5m Ultra-stable CFRS Antenna Reflector Matthias Friemel - Large Space Structures UG
11:40 - 12:00 - Technology and Dimensional Stability Demonstration of a 5m Shell-Membrane Large Deployable Antenna Reflector Leri Datashvili - Large Space Structures UG

Chair: J. Buffe & R. Usinger

Cassiopée

10:40 - 11:00 - Design Loads Definition and Mechanical Verification for the Euclid Spacecraft Adriano Calvi - European Space Agency
11:00 - 11:20 - Crushable TPS - From dynamic characterization of material crash behavior up to tests at scale one Jerome Mespoulet - THIOT INGENIERIE
11:20 - 11:40 - Mechanical architecture discoupling Guillaume Couderc - Airbus D&S - TSOTD7
11:40 - 12:00 - Development and testing of equipment attachment zones for lattice and grid-stiffened composite structures Leonid Pavlov - ATG Europe

Chair: Q. Shi & A. Grillenbeck

Guillaumet 2

10:40 - 11:00 - EXOMARS SCC MECHANICAL QUALIFICATION TEST CAMPAIGN Stefano Destefanis - THALES ALENIA SPACE ITALIA
11:00 - 11:20 - IXV Mechanical Test Campaign Stefano Destefanis - THALES ALENIA SPACE ITALIA
11:20 - 11:40 - Testing the LISA Pathfinder test mass uncaging and injection into a geodesic Daniele Bortoluzzi - University of Trento
11:40 - 12:00 - AIT Challenges during Environmental Testing of an Electric Propulsion Subsystem at Satellite level David Leoty - OHB System AG
12:00 - 12:20 - Experimental Investigations on dynamic aeroelastic Stability of Panels in The Transonic Domain Jannis Lübker - DLR, German Aerospace Center

Chair: R. Bureo Dacal & T. Henriksen

Guillaumet 1

10:40 - 11:00 - Design and validation of a test bench for cryocooler induced microvibration measurements Lopes Diogo - AirLiquide Advanced Technologies
11:00 - 11:20 - New experimental test to characterize bonding shock resistance Marina Voisin - LMA
11:20 - 11:40 - Representative mechanical shock testing for satellite electronic units Joey Poirier - Thales Alenia Space France
11:40 - 12:00 - Shock prediction at satellite level Nicolas Coral - MECANO ID
12:00 - 12:20 - Pyrotechnic Shock Scaling Method Using Statistical Energy Analysis James Hwang - MIT Lincoln Laboratory

Chair: A. Carrella & C. Puillet

Guillaumet 1

13:40 - 14:00 - Vibration Testing of the Eu:CROPIS Satellite Test Structure Olaf Mierheim - DLR (German Aerospace Center)
14:00 - 14:20 - Acoustic analysis and testing of the Hispasat AG1 satellite Proto-Flight Model Florian Ruess - Space Structures GmbH
14:20 - 14:40 - Vibrations: What's behind the curves? Robert Knockaert - European Space Agency

Chair: M. Straubel & C. Dupuy

Spot

13:40 - 14:00 - Dynamics of Curved Bistable Reeled Composites Geoffrey Knott - University of Surrey
14:00 - 14:20 - Design and Analysis for An Elliptical Ring Truss Reflector Qingzheng Song - Shanghai YS Information Technology Co., Ltd.
14:20 - 14:40 - METHOD OF EVALUATION OF SMALL ASYMMETRY IMPACT ON LONGITUDINAL AXIS DEVIATIONS FROM SPACE LANDING VEHICLE WITH INFLATABLE BRAKING DEVICE UNDER CONDITIONS OF RESONANCE MODES OF MOVEMENT Koryanov Vsevolod - Bauman Moscow State Technical University
14:40 - 15:00 - Origami-inspired Shape Memory Dual-Matrix Composite Structures Jin-Ho Roh - Korea Aerospace University

Chair: S. Roose & A. Grillenbeck

Guillaumet 2

13:40 - 14:00 - Results of the end to end calibration of a thermal measurement system for the LSS (NgDCU) Alessandro Cozzani - esa estec
14:00 - 14:20 - Adaptation of an Auxiliary Thermal-Vacuum Chamber for Testing Fabien Cabaret - INTESPACE
14:20 - 14:40 - Wide Range Thermal Test Facility for Juice Large Appendages Christophe Grodent - Centre Spatial de Liège
14:40 - 15:00 - Improved Sun Simulation at High Flux Level Paul-Eric Dupuis - INTESPACE

Chair: E. Standarovski & T. Henriksen

Cassiopée

13:40 - 14:00 - STUDY OF THE DYNAMICS OF LANDING A SPACECRAFT ON A SMALL CELESTIAL BODY UNDER FIXING CONDITIONS Koryanov Vsevolod - Bauman Moscow State Technical University
14:20 - 14:40 - Mechanical sizing of a sub-system at an optimized system level D. Renio - Thalesaleniaspace
14:40 - 15:00 - Support System Development of the HP3 Instrument for the Mars Mission InSight Siebo Reershemius - German Aerospace Center (DLR)
15:00 - 15:20 - Semi-Automated Mechanical Analysis of Large Scale Line Routings in Modern Spacecraft Robert Meitzner - Airbus Defence and Space

Chair: A. Cozzani & S. Roose

Guillaumet 2

15:20 - 15:40 - AIT Challenges in Environmental Testing: Thermal Vacuum Testing Carsten Reese - OHB System AG
16:20 - 16:40 - Thermal-Vacuum Chamber Refurbishment Remi Lamande - INTESPACE
16:40 - 17:00 - Thermal Vacuum Test Methods for BepiColombo Mercury Mission Georg Deutsch - European Test Services (ETS)
17:00 - 17:20 - Integration of IR thermography into thermal-vacuum test facilities: a keep-it-simple approach. Peter Jens Hein - IABG
17:20 - 17:40 - Atmospheric entry of space debris: influence of oxidation and emissivity in the calculation of the spacecraft survivability Marianne Balat-Pichelin - PROMES-CNRS
17:40 - 18:00 - Estimation of environmental influence on spacecraft materials radiative properties Aleksey Nenarokomov - Moscow Aviation Institute

Chair: A. Kiley & B. Gergonne

Spot

16:20 - 16:40 - Strategy of pressing load adjustment for high precision positioning mechanism using Kinematic Coupling Takagi Kentaro - National Defense Academy of JAPAN
17:00 - 17:20 - Evaluation of Different Architectural Concepts for Huge Deployable Solar Arrays for Electric Propelled Space Crafts Marco Straubel - DLR
17:20 - 17:40 - Design, Analysis and Testing of the ADEO Passive De-Orbit Subsystem Demonstrator Thomas Sinn - HPS GmbH
17:40 - 18:00 - Development of Shape Memory Polymer Composites for Space Deployable Structures Yanping Yanping Song - Xi'an Institute of Space Radio Technology

Chair: R. Bureo Dacal & J. Buffe

Cassiopée

16:20 - 16:40 - Development of mass and cost efficient grid-stiffened and lattice structures for space applications Leonid Pavlov - ATG Europe
16:40 - 17:00 - Ice Cloud Imager (ICI) mechanical architecture Sanchez-Pascuala Daniel - Airbus Defence & Space
17:00 - 17:20 - Ku-Band Dual-Gridded Carbon Fibre Reinforced Plastic Reflector Olaf Reichmann - HPS GmbH
17:20 - 17:40 - An Overview on Prediction of Damping Characteristics of the Satellites With Respect to the Environmental Tests Performed on Structural Qualification Models Baris Eroglu - TAI - Turkish Aerospace Industries, Inc.
17:40 - 18:00 - Aeroelastic Instabilities Analysis of Elastic and Viscoelastic Multi-Layered Panels Zappino Enrico - Politecnico di Torino

Chair: J. Martin Llorente & C. Huehne

Guillaumet 1

16:20 - 16:40 - New Materials For Passive Damped Deployment Of Full Composite Structures Nieto Jose - COMET Ingeniería
16:40 - 17:00 - Simulation and measurement of thermal fluxes in load-bearing bonded FRP single-lap joints Michael Lange - DLR - German Aerospace Center
17:00 - 17:20 - Innovation in Automated Insert Potting for Space Applications Alexandra Isele - RUAG Space
17:20 - 17:40 - Space struts trade off following different needs Yohann Ledru - MECANO ID
17:40 - 18:00 - Determination of stable and robust material properties for the assessment of thermomechanically loaded components of rocket engines with viscoplastic constitutive equations Thomas Seifert - Offenburg University of Applied Sciences

Chair: A. Cozzani & J. Buffe

Guillaumet 2

08:30 - 08:50 - Sensors Network Development Paul-Eric Dupuis - INTESPACE
08:50 - 09:10 - Development of a Fully Automatic Data Acquisition and Control System for Testing Space Mechanisms Irina KUPETZ - RUAG Schweiz AG - RUAG Space
09:10 - 09:30 - Sensor Numerical Identification Paul-Eric Dupuis - INTESPACE
09:30 - 09:50 - 6 Degree of Freedom Micro-Vibration Test Facility for European Space Agency Charlie Jarvis - National Physical Laboratory
09:50 - 10:10 - Performance validation of a Verstaile Vibration Isolation System for Micro-Vibration studies Francois Decobert - SEREME

Chair: R. Bureo Dacal & C. Puillet

Guillaumet 1

08:30 - 08:50 - Component Mode Synthesis model reduction for acoustic models Simon Appel - ESA
08:50 - 09:10 - Acoustic Response of Spacecraft Equipment and Shock Response from SEA Prediction Gerard Borello - InterAC
09:10 - 09:30 - SpaceBus NEO - Random Specification Through Acoustic Analyses D. Renio - Thales Alenia Space
09:30 - 09:50 - Derivation of Mass Acceleration Curve Based on Acoustic Test Measurement Data of JAXA Spacecraft Shingo Shimazaki - Japan Aerospace Exploration Agency (JAXA)
09:50 - 10:10 - Predicting the vibroacoustic response of spacecraft using the Coupled Multilevel Fast Multipole Method, a High-speed Boundary Element Method Nicolas Zerbib - ESI GROUP

Chair: A. Hot & M. Vorel

Spot

08:30 - 08:50 - Verification of ceramic structures: qualification and proof testing Fabrice Blanc - Thales Alenia Space France
08:50 - 09:10 - Ceramic space structures sizing and verification: handbook development and upcoming investigations David Denaux - Airbus Defence and Space
09:10 - 09:30 - Recent advances on fast fracture strength of Zerodur® for space applications Stéphanie Behar-Lafenetre - Thales Alenia Space France
09:30 - 09:50 - Sub-critical crack growth of Zerodur® Stéphanie Behar-Lafenetre - Thales Alenia Space France
09:50 - 10:10 - Fatigue of a ceramic matrix composite sample in high temperature conditions Daniel Vaucher De La Croix - ACOEM

Chair: P. Mourey & J. Martin Llorente

Cassiopée

08:50 - 09:10 - Mass and cost efficient launcher structures thanks to structural optimization methods Lander Ruiz De Ocenda - CNES - Centre National d'Etudes Spatiales
09:10 - 09:30 - Innovative cork application on a thermal deflector for apogee boost motors Joao Ricardo - Active Space Technologies, S.A.
09:30 - 09:50 - Novel Hypersonic Launcher Concept using Thin-Ply CFRP Technologies Alexander Kopp - German Aerospace Center DLR

Chair: A. Cozzani & J. Buffe

Guillaumet 2

10:40 - 11:00 - BepiColombo MPO PFM Radiated EMC Test with dedicated MGSE Georg Deutsch - European Test Services (ETS)
11:00 - 11:20 - Guidelines of a metamaterial for launcher tanks dynamic experiments Edith Grippon - DyanS+
11:20 - 11:40 - Vibrational test bench of a grain filled tank in view of cryogenic tank test Pierre-Louis Chiambaretto - ISAE-SUPAERO

Chair: P. Mourey & M. Vorel

Cassiopée

10:40 - 11:00 - Anisogrid Payload Adaptor Structure for Vega Launcher Carlos B. Mangas Calvo - Airbus Defence & Space
11:00 - 11:20 - Design and Analysis of Launcher Tanks with Bolted Joints Jacques Marchesini - INTES France
11:20 - 11:40 - Universal Low Cost Secondary Payload Adapters for European Launchers Lander Ruiz De Ocenda - CNES - Centre National d'Etudes Spatiales
11:40 - 12:00 - Progress on Advanced Cryo-Tanks Structural Design Achieved in CHATT-project Alexander Kopp - DLR-SART

Chair: P. Corberand & C. Puillet

Guillaumet 1

10:40 - 11:00 - Adhesive Free High Stability Optical Mount for Space Laser Applications Mosciarello Paolo - Finmeccanica Airborne and Space Systems Division
11:00 - 11:20 - Design, Development and Verification of the Merlin Payload Stefano Lucarelli - Airbus Defence & Space
11:20 - 11:40 - Mechanical architecture of the MTG instruments supporting structure (FCI-TA & IRS) Elguea Mikel - AirbusDS
11:40 - 12:00 - Lightweight All-CFRP Struts with Near Zero CME and CTE Niels Christian Jessen - Danish Technical University Space
12:00 - 12:20 - MTG INSTRUMENTS: MECHANICAL DESIGN SOLUTIONS FOCUSED ON THE STRUCTURE THERMOELASTIC BEHAVIOUR AND THE SENSITIVITY ON THE OPTICAL PERFORMANCES. Gonzalo Galvez Soler - Airbus DS

Chair: J. Martin Llorente & C. Huehne

Spot

11:00 - 11:20 - Nano-enabled composites for space applications: a review of latest achievements under ESA activities Athanassios Baltopoulos - Adamant Composites Ltd
11:20 - 11:40 - Sulfur Concrete – Promising Material for Space-Structures Building Rafał Anyszka - Lodz University of Technology, Institute of Polymer and Dye Technology
11:40 - 12:00 - Real prediction of ground ageing of materials used in space industry by thermokinetic analysis Christian Puig - AIRBUD DS

Chair: C. Puillet & M. Appolloni

Guillaumet 2

13:40 - 14:00 - Damage tolerance and LCF behaviour of TA6V-SLM Farhad Rezai-Aria - Institut Clement Ader Site-Mines Albi C
14:00 - 14:20 - Modified Spectral Fatigue Methods for S-N Curves with MIL-HDBK-5J Coefficients Irvine Tom - Dynamic Concepts Inc
14:20 - 14:40 - Life time prediction of rocket combustion chambers – current justification approaches per analysis and test Marcus Lehmann - Airbus DS
14:40 - 15:00 - Relationship between damage and permeability in liner-less composite tanks: experimental study at the lamina level Hortense Laeuffer - CNES
15:00 - 15:20 - Delamination Assessment Tool for Composite Structures Celeste Pereira - HPS - High Performance Structures, Gestão e Engenharia Lda

Chair: R. Usinger & J. Martin Llorente

Cassiopée

13:40 - 14:00 - Industrial equivalent modelling of a screw assembly subjected to a thermal load Rémi Thanwerdas - Icam
14:00 - 14:20 - Opto-Mechanical Optimisation Alexis Blot - Airbus DS
14:20 - 14:40 - Design and optimized sizing of composite structures: focus on composite winding pressurized structures Kévin Mathis - CNES - Launchers Directorate
14:40 - 15:00 - Sentinel-1C&D: A novel approach to space debris mitigation Mathias Alberti - Airbus DS GmbH
15:00 - 15:20 - Sentinel-1C&D: Antenna separation mechanism for safe de-orbiting Mathias Alberti - Airbus DS GmbH

Chair: J. Buffe & A. Hot

Spot

13:40 - 14:00 - ARIANE 6 loads and environment - Coupled optimization process and System analyses, supporting requirements vs design convergence loop involving EU Partners Poupard Leny - Airbus Defence and Space
14:00 - 14:20 - New Approaches for Reliability Assessment of Mechanical Systems and Parts (Part 1 – Methodology) Katharina Fischer - Matrisk GmbH
14:20 - 14:40 - New Approaches for Reliability Assessment of Mechanical Systems and Parts (Part 2 – Case Study) Nikolay Asmolovskiy - Space Structures GmbH
14:40 - 15:00 - Multiscale analysis of uncertainties in lightweight structures consisting of materials with uncertain microstructure Jörg Hohe - Fraunhofer Institut für Werkstoffmechanik IWM
15:00 - 15:20 - Robust test design for spacecraft mechanical testing Fabien Maugan - FEMTO-ST

Chair: P. Mourey & G. Ladurée

Guillaumet 1

13:40 - 14:00 - Measurement and Simulation of Damping Properties of Spacecraft Structure Components under Microvibration Loads Robert Hahn - Hoch Technologie Systeme GmbH
14:00 - 14:20 - Assessment of actual boundary conditions affecting numerical buckling prediction due local cutouts Kaspars Kalnins - Riga Technical University
14:20 - 14:40 - A method for local damping identification Marc Böswald - DLR - Institute of Aeroelasticity
14:40 - 15:00 - Crushable TPS - Crash behavior predictions and correlation Sophie Allee - MECANO ID
15:00 - 15:20 - Analysis of composite launcher with non-structural masses subjected to loading factor Tommaso Cavallo - Politecnico di Torino
15:20 - 15:40 - Structural Dynamics and Control Implications for Modal Damping of a Simplified Two-Blade Heliogyro Model Sarah COOK - University of Colorado at Boulder

Chair: P. Corberand & S. Fransen

Spot

16:20 - 16:40 - Thermo-elastic tests of the LISA Telescope Assembly: main results and lessons learnt Stefano Lucarelli - Airbus Defence & Space
16:40 - 17:00 - Development of Self-Sensing Truss for Thermally Stable Spacecraft Structures Kazuya Kitamoto - Japan Aerospace Exploration Agency
17:00 - 17:20 - A Multidisciplinary Software for Structural, Thermal and ‎Optical Performance Analysis of Space Optical Instruments Alexander Kuisl - OHB System AG

Chair: P. Hein & V. Koryanov

Guillaumet 2

16:20 - 16:40 - Qualification Testing of the Gossamer-1 Deployment Technology Tom Sproewitz - German Aerospace Center
16:40 - 17:00 - Preliminary Creep Test for estimating the long term stowage behavior of DLR’s CFRP booms Sebastian Meyer - DLR - German Aerospace Center
17:00 - 17:20 - Large Stable Deployable Structures for Future Science Missions Celeste Pereira - HPS - High Performance Structures, Gestão e Engenharia Lda
17:20 - 17:40 - Deployable morphing structure using double cylindrical tube Atsushi Aso - National Defense Academy of Japan

Chair: A. Carrella & C. Huehne

Cassiopée

16:20 - 16:40 - Life span modelling of ultra-thin CFRP masts subjected to accelerated environmental ageing Agnieszka Suliga - University of Surrey
16:40 - 17:00 - HiTOS: an Optical-Fibre based High Temperature Sensor for Space Vehicles applications. Francisco García-de-Quirós - Emxys
17:00 - 17:20 - Metallic surfaces under interplanetary medium – degradation mechanisms and protection possibilities Maciej Sznajder - German Aerospace Center (DLR)
17:20 - 17:40 - Emergence of Airware 2050 for space launch cryogenic tankage applications Michael Niedzinski - Constellium

Chair: R. Bureo Dacal & I. Ngan

Guillaumet 1

16:20 - 16:40 - Comparison of models for spacecraft space debris vulnerability analyses Christian Puillet - CNES
16:40 - 17:00 - Development of a Velocity Amplification Module for millimeter size hypervelocity impacts between 8 and 12 km/s Jerome Mespoulet - THIOT INGENIERIE
17:00 - 17:20 - Experimental and numerical study of submillimetric hypervelocity impacts on honeycomb sandwich structures Paul Deconinck - THIOT INGENIERIE
17:20 - 17:40 - INNOVATIVE MODELING IN HYPERVELOCITY IMPACTS Jean-Luc Lacome - IMPETUS
17:40 - 18:00 - Blast and impact loading on cylindrical and conical shells: application for space launcher structures Benoit Tang - CNES - French Space Agency

Chair: M. Straubel & C. Puillet

Spot

08:30 - 08:50 - Design of an experimental set-up to analyse compliant mechanisms used for the deployment of a panel Florence Dewalque - University of Liège
08:50 - 09:10 - RITD project - the technology applying of inflatable devices to access adaptation, movement and landing descent vehicle from Martian environment to the Earth considering the influence of different environmental conditions Koryanov Vsevolod - Bauman Moscow State Technical University
09:10 - 09:30 - LAGARD: A European Modular Large Stable Deployable Structure Vlachos Dimitris - Adamant Composites Ltd
09:30 - 09:50 - Mechanical testing of deployable thin shell CFRP booms in ideal and realistic interfaces for the Solar Sail Demonstrator Gossamer-1 Zander Martin - German Aerospace Center - DLR & TU Braunschweig
09:50 - 10:10 - Super-pressure balloon clefting Bouzidi Rabah - Nantes University

Chair: Q. Shi & R. Bureo Dacal

Guillaumet 1

08:30 - 08:50 - Experimental Validation of Direct Field Acoustic Testing Christophe Fabries - THALES ALENIA SPACE
08:50 - 09:10 - Development of a new powerful acoustic modulator Florent Haddad - INTESPACE
09:10 - 09:30 - Direct Field Testing Simulation for Subsystem Acoustic Qualification Christophe Fabries - THALES ALENIA SPACE
09:30 - 09:50 - Industrial verification of projection algorithms and optimization routines for acoustic field uniformity enhancement in MIMO direct field acoustic control Mariano Alvarez Blanco - Siemens Industry Software NV
09:50 - 10:10 - Feedforward control of acoustic tests Sebastian Wezenbeek - TU Delft

Chair: R. Usinger & M. Jacquesson

Cassiopée

08:30 - 08:50 - Mechanical behavior of polyamide 12 fabricated via selective laser sintering : Experimental investigations, modeling and validation through an aerospace structure mechanical test Emmanuel Dumoulin - Dassault-Aviation
08:50 - 09:10 - Engineering design cycle for an ALM Secondary structure, from concept to final validation. Example of the flight proven aluminum (AS7G06) part. Marion Salvi - Thales Alenia Space
09:10 - 09:30 - Quality Control of a Metallic Additive Layer Manufacturing Part thanks to X-ray Computerized Tomography and Finite Element Modeling Julien Uzanu - ELEMCA
09:30 - 09:50 - Designing metallic AM components for space structures. Practical cases for a challenging implementation in flight H/W Jorge Vilanova - AIRBUS DEFENCE & SPACE EADS CASA Espacio
09:50 - 10:10 - Metallic lattice material in additive manufacturing for satellite structural parts Franck Leid - MECANO ID

Chair: A. Cozzani, M. Appolloni, R. Knockaert

Guillaumet 2

08:30 - 08:50 - Spacecraft Vibration Testing: Benefits and Potential Issues Ali Kolaini - JPL NASA
08:50 - 09:10 - Transient Testing from LV/SC Coupled Analysis by new Shock Synthesis Alain GIRARD - INTESPACE
09:10 - 09:30 - Implementation and test of a robust mass operator tool Raymond Olympio - Airbus DS GmbH
09:30 - 09:50 - Sine Sweep Effect on Specimen Modal Parameters Characterization Nicolas Roy - Top Modal
09:50 - 10:10 - A Virtual Testing Approach for Spacecraft Structures Post-Correlation Purposes Remedia Marcello - Surrey Space Centre (University of Surrey)

Chair: R. Bureo Dacal & J. Buffe

Spot

10:40 - 11:00 - Vibration isolators for space applications – various configurations Gilles Carte - Thales Alenia Space France
11:00 - 11:20 - Insight NASA Program : Damping isolators of the SEIS Instrument Tony Demerville - SMAC
11:20 - 11:40 - Design and analysis of a novel 2-collinear-DoF strut with embedded electromagnetic shunt dampers Alessandro Stabile - Surrey Space Centre (University of Surrey)
11:40 - 12:00 - SAFE :Shock Attenuator For Equipment Tony Demerville - SMAC
12:00 - 12:20 - Active vibration isolation of launcher vibration environment Christophe Collette - Université Libre de Bruxelles

Chair: Q. Shi & I. Ngan

Guillaumet 1

10:40 - 11:00 - How NGTD helps improving vibroacoustic calculation in time domain Daniel Vaucher De La Croix - ACOEM
11:00 - 11:20 - Stochastic FEM-BEM Method for Spacecraft Vibroacoustic Analysis Vladimir Yotov - Surrey Space Centre, University of Surrey
11:20 - 11:40 - Robust vibro-acoustic analysis in the low and mid-frequency range of spacecraft payloads submitted to diffuse sound field excitation Benoit Van Den Nieuwenhof - Free Field Technologies, MSC Software Company
11:40 - 12:00 - Comparison of vibro-acoustic test results and predictions using the boundary element method Arnaud Chiri - Airbus Defence and Space GmbH
12:00 - 12:20 - Determination of loss factors through experimental SEA for systems with restricted accessibility Chimeno Marcos - Technical University of Madrid

Chair: R. Usinger & M. Jacquesson

Cassiopée

10:40 - 11:00 - Maturation of Additive Manufacturing for Implementation into ARIANE Secondary Structures: Overview and Status of "ALM ISCAR" Sebastian Kébreau - Airbus Defence and Space
11:00 - 11:20 - 3D printing optimized design applied to a Taranis satellite part Paul Mirguet - SOGECLAIR aerospace
11:20 - 11:40 - Rapid Design and Build Technology for Small Satellite Applications Hamar Chris - Surrey Satellite Technology Limited
11:40 - 12:00 - Additive Manufacturing Hot Bonded inserts in sandwich structures Marta Garcia-Cosio - Atos
12:00 - 12:20 - End-to-End part development: a case study how to use Additive Manufacturing to realise components within a tight project time-line Michael Gschweitl - RUAG Schweiz AG, RUAG Space

Chair: A. Cozzani, M. Appolloni, R. Knockaert

Guillaumet 2

10:40 - 11:00 - Numerical Modelling and Simulation of a Closed-Loop Electrodynamic Shaker and Test Structure Model for Spacecraft Vibration Testing Steffen Waimer - Siemens Industry Software NV
11:00 - 11:20 - Feasability of the beating cancellation during the satellite vibration test Alain Bettacchioli - THALES ALENIA SPACE
11:20 - 11:40 - Utilizing virtual vibration tests to optimize physical shaker tests Frédéric Kihm - HBM nCode products
11:40 - 12:00 - A VIRTUAL SHAKER TESTING EXPERIENCE: MODELING, COMPUTATIONAL METHODOLOGY AND PRELIMINARY RESULTS Pietro Nali - TAS-I
12:00 - 12:20 - Investigations Concerning the Effectiveness of the Spacecraft Finite Element Model Correlation and Update Process Judith Mercer - University of Surrey

Chair: A. Cozzani, M. Appolloni, R. Knockaert

Guillaumet 2

13:40 - 14:00 - Nonlinear Vibration Analysis of the SmallSat Spacecraft: From Identification to Design Thibaut Detroux - University of Liege
14:00 - 14:20 - Static and dynamic load superposition in spacecraft structural analysis Xavier VAQUER ARAUJO - Airbus DS GmbH Friedrichshafen

Chair: G. Piret & P. Mourey

Spot

13:40 - 14:00 - Passive solution for spacecraft internal damping Gwenaelle Aridon - Airbus Defense & Space
14:00 - 14:20 - Experimental analysis of linear vibration absorbers for an uncertain main structure Guilhem Michon - Université de Toulouse - ICA ,CNRS, ISAE
14:20 - 14:40 - Damping Insert TARANIS Maxime Brel - AIRBUS DS
14:40 - 15:00 - SEPARFACE: Innovative technology for elastomer molding Guy Aubert - EFJM

Chair: R. Bureo Dacal & C. Puillet

Guillaumet 1

13:40 - 14:00 - Sound Transmission Loss through honeycomb sandwich panels: prediction and parametric survey Zakaria Zergoune - école centrale de Lyon
14:00 - 14:20 - The reconsideration on test effectiveness by reverberant acoustic test from the point of view on vibration responses to different sound include flight measurement Qinzhong Shi - Japan Aerospace Exploration Agency (JAXA)
14:20 - 14:40 - Acoustic and random vibration tests margin investigation by reviewing fatigue damage of flight and ground test Takafumi Kajikawa - Japan Aerospace Exploration Agency (JAXA)
14:40 - 15:00 - Propulsion Tubing Optimised Sizing Through Acoustic Analyses Jean-Claude Renault - ThalesAleniaSpace

Chair: R. Usinger & M. Jacquesson

Cassiopée

13:40 - 14:00 - Measurement of Fracture Toughness of Metallic Materials Produced by Additive Manufacturing Philippe Guy - Icam
14:00 - 14:20 - ADDITIVE MANUFACTURED METALLIC FLEXIBLE STRUCTURES, A FOCUS ON MANUFACTURING STRATEGIES, MATERIAL ANALYSIS AND FATIGUE VERIFICATION Hervé Saudan - CSEM SA - Centre Suisse d'Eletronique et de Microtechnique SA
14:20 - 14:40 - Qualification of AM parts: the application of extreme value statistics for volumetric defect analysis Romano Simone - Politecnico di Milano
14:40 - 15:00 - Stress Corrosion Cracking Behaviour and Microstructural Characteristics of Scalmalloy Manufactured by Selective Laser Melting Mozdzen Grazyna - Aerospace & Advanced Composites GmbH
15:00 - 15:20 - Use of Laser Metal Deposition (LMD) for Spacecraft Structural Parts Production Bernard Gergonne - Airbus Defence & Space